Consider flow of air over a flat plate. On one graph, plot the laminar boundary-layer thickness as a function of distance along the plate (up to transition) for freestream speeds \(U=1 \mathrm{~m} / \mathrm{s}, 2 \mathrm{~m} / \mathrm{s}\), \(3 \mathrm{~m} / \mathrm{s}, 4 \mathrm{~m} / \mathrm{s}, 5 \mathrm{~m} / \mathrm{s}\), and \(10 \mathrm{~m} / \mathrm{s}\).